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TEKA0007404, Tekniska museet, Sweden

The recent testing for the Graflight V-8, a high-efficiency,

Fire truck engine usage training

Ten Arm Owens Automatic Bottle Machine. Courtesy of Owen's Automatic Bottle Machine Co., Toledo, Ohio. Location: Toledo, Ohio

P-40 STIRLING ENGINE INSTALLATION

US Air Force (USAF) AIRMAN First Class (A1C) Nicholas Charles, 86th Maintenance Squadron (MXS), operates an electrical hoist to position a Reduction Gearbox onto a maintenance stand, inside the maintenance shop at Ramstein Air Base (AB), Germany

Air crews at Air Station Elizabeth City load a HC-130J

200424-N-MQ631-0027 ATLANTIC OCEAN (April 24, 2020)

code Related

HIGH PRESSURE HIGH TEMPERATURE COMBUSTOR

HIGH PRESSURE HIGH TEMPERATURE COMBUSTOR

HIGH PRESSURE COMBUSTOR, NASA Technology Images

HIGH PRESSURE HEAT TRANSFER RIG

HIGH PRESSURE COMBUSTOR, NASA Technology Images

HIGH PRESSURE HEAT TRANSFER RIG

HIGH PRESSURE HEAT TRANSFER RIG

HIGH PRESSURE HEAT TRANSFER RIG

HIGH PRESSURE COMBUSTOR HARDWARE, NASA Technology Images

HIGH PRESSURE HIGH TEMPERATURE COMBUSTOR

description

Summary

The original finding aid described this as:

Capture Date: 1/24/1975

Photographer: DONALD HUEBLER

Keywords: Larsen Scan

Location Building No: 102

Location Room: ECRL-1

Photographs Relating to Agency Activities, Facilities and Personnel

Nothing Found.

label_outline

Tags

high pressure temperature combustor nasa national aeronautics and space administration high resolution ultra high resolution high pressure high temperature combustor ecrl 1 photographs location room photographer donald huebler nasa photographs 1970 s space program us national archives
date_range

Date

1975
create

Source

The U.S. National Archives
link

Link

https://catalog.archives.gov/
copyright

Copyright info

No known copyright restrictions

label_outline Explore Ecrl 1 Photographs, Combustor, Pressure

A man works to install a submarine emergency communication transmitter (SEC) buoy Mark 9 Mod O outside the pressure hull and inside the other hull of a simulated submarine hull section during testing at the Naval Ordnance Laboratory. When put into fleet use the SECT will be released and act as a surface marker if and when the ship is sunk

ENGINE RESEARCH BUILDING ERB 8X11 TEST CELL SE-6 AND TEST CELL SE-4 CONTROL ROOM

2 HIGH TEMPERATURE PRESSURE FURNACES IN THE MATERIALS AND STRESSES M&S BUILDING ROOM 31

PRESSURE SYSTEMS - HIGH PRESSURE AIR SYSTEMS - NITROGEN PURGE - 450 COMBUSTION AIR

S130E009086 - STS-130 - Node 3 Deck Alcove Internal View

SWITCH GEAR IN THE CENTER SECTION

HIGH POWER AMPLIFIER TUBE LITTON MODEL 2005-R3

PLASTIC COMBUSTOR MODEL, NASA Technology Images

CRT C2 CARBON DIOXIDE PRIMARY COMBUSTOR SECTION

Spaceward Bound event in the Mojave Deser , CA (an outreach exercise) with Dr Chris McKay and Ames Education department personnel Brian Day, Barbara Bazar and a accompaning (learning for the the classroom) team of teachers will be studying side-by-side with NASA scientists who search for life in extreme environments, closely approximating what they expect to find on other planets. Why the Mojave -- an inhospitable, sun-drenched spot in the California Desert? This natural setting presents scientists with opportunities to study environments that are analogous to what explorers will find on the Moon and Mars. Teachers and scientists will perform scientific fieldwork in lunar geology, Mars astrobiology, Mars geology, and issues of temperature and solar inundation and radiation. for additional information and Outreach projects see http://quest.arc.nasa.gov/ ARC-2007-ACD07-0056-085

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Dan Kenna (right) positions a Reinforced Carbon Carbon panel on the table to perform flash thermography. In the background, Paul Ogletree observes the monitor. Attached to the leading edge of the wing of the orbiters, the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot. The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

J85 IN PROPULSION SYSTEMS LABORATORY PSL TANK 3 - TF34 ENGINE IN MIDDLE OF FLOOR

Topics

high pressure temperature combustor nasa national aeronautics and space administration high resolution ultra high resolution high pressure high temperature combustor ecrl 1 photographs location room photographer donald huebler nasa photographs 1970 s space program us national archives